EP2354518A3 - Procédé de fabrication d'une tuyère divergente à refroidissement régénératif d'une chambre de combustion de moteur-fusée et tuyère - Google Patents
Procédé de fabrication d'une tuyère divergente à refroidissement régénératif d'une chambre de combustion de moteur-fusée et tuyère Download PDFInfo
- Publication number
- EP2354518A3 EP2354518A3 EP11000944.6A EP11000944A EP2354518A3 EP 2354518 A3 EP2354518 A3 EP 2354518A3 EP 11000944 A EP11000944 A EP 11000944A EP 2354518 A3 EP2354518 A3 EP 2354518A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- nozzle
- wall
- combustion chamber
- manufacturing
- rocket combustion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 title abstract 2
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 238000001816 cooling Methods 0.000 abstract 4
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D39/00—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
- B21D39/03—Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of sheet metal otherwise than by folding
- B21D39/031—Joining superposed plates by locally deforming without slitting or piercing
- B21D39/032—Joining superposed plates by locally deforming without slitting or piercing by fitting a projecting part integral with one plate in a hole of the other plate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/008—Rocket engine parts, e.g. nozzles, combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/97—Rocket nozzles
- F02K9/972—Fluid cooling arrangements for nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49346—Rocket or jet device making
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010007272.9A DE102010007272B4 (de) | 2010-02-08 | 2010-02-08 | Verfahren zur Herstellung einer regenerativ gekühlten Düsenerweiterung einer Raketenbrennkammer und Düsenerweiterung |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2354518A2 EP2354518A2 (fr) | 2011-08-10 |
EP2354518A3 true EP2354518A3 (fr) | 2014-02-26 |
EP2354518B1 EP2354518B1 (fr) | 2014-11-05 |
Family
ID=43618117
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11000944.6A Active EP2354518B1 (fr) | 2010-02-08 | 2011-02-07 | Procédé de fabrication d'une tuyère divergente à refroidissement régénératif d'une chambre de combustion de moteur-fusée et tuyère |
Country Status (3)
Country | Link |
---|---|
US (1) | US20110192137A1 (fr) |
EP (1) | EP2354518B1 (fr) |
DE (1) | DE102010007272B4 (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10343049B3 (de) * | 2003-09-16 | 2005-04-14 | Eads Space Transportation Gmbh | Brennkammer mit Kühleinrichtung und Verfahren zur Herstellung der Brennkammer |
CN103707010B (zh) * | 2013-12-12 | 2016-01-20 | 西安航天动力机械厂 | 一种无底球冠形零件制造方法 |
CN105710606A (zh) * | 2015-11-25 | 2016-06-29 | 沈阳黎明航空发动机(集团)有限责任公司 | 一种燃气发生器喷嘴头的加工方法 |
DE102016212314B4 (de) * | 2016-07-06 | 2022-05-12 | Arianegroup Gmbh | Verfahren zur Herstellung einer Brennkammer |
CN106423597A (zh) * | 2016-10-28 | 2017-02-22 | 北京航天动力研究所 | 一种铣槽扩散焊喷嘴 |
US9835114B1 (en) | 2017-06-06 | 2017-12-05 | The United States Of America As Represented By The Administrator Of Nasa | Freeform deposition method for coolant channel closeout |
CN109079322A (zh) * | 2018-07-11 | 2018-12-25 | 陕西蓝箭航天技术有限公司 | 航天运载器的发动机喷管制备方法 |
CN112431687B (zh) * | 2020-11-12 | 2022-07-08 | 太原科技大学 | 一种折叠式轨控发动机高温隔热机构 |
US11779985B1 (en) * | 2020-11-15 | 2023-10-10 | Herbert U. Fluhler | Fabricating method for low cost liquid fueled rocket engines |
KR102468746B1 (ko) * | 2020-11-18 | 2022-11-18 | 한국항공우주연구원 | 열교환 구조를 포함하는 연소기 및 이를 포함하는 로켓 |
DE102020133967A1 (de) | 2020-12-17 | 2022-06-23 | Arianegroup Gmbh | Brennkammer, Verfahren zur Herstellung einer Brennkammer und Triebwerk |
CN115302209B (zh) * | 2022-10-12 | 2023-01-13 | 北京智创联合科技股份有限公司 | 通过内外壁一体成形方案制造火箭发动机喷管的方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3613207A (en) * | 1969-06-05 | 1971-10-19 | Messerschmitt Boelkow Blohm | Method for covering and closing cooling channels of a combustion chamber |
FR2311608A2 (fr) * | 1975-05-22 | 1976-12-17 | Messerschmitt Boelkow Blohm | Procede de realisation de pieces de revolution, notamment refroidies par un liquide, comme des tuyeres et chambres de combustion pour moteurs-fusees |
FR2774432A1 (fr) * | 1998-02-04 | 1999-08-06 | Daimler Benz Ag | Chambre de combustion pour des moteurs et des tuyeres de forte puissance |
WO2000032920A1 (fr) * | 1998-11-27 | 2000-06-08 | Volvo Aero Corporation | Structure tuyere pour cols de tuyeres avec paroi refroidie |
US6998570B1 (en) * | 2004-11-04 | 2006-02-14 | United Technologies Corporation | Beam welding apparatus and methods |
US20070259192A1 (en) * | 2006-05-08 | 2007-11-08 | Eads Space Transportation Gmbh | Method for producing components for rocket construction |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4304821A (en) * | 1978-04-18 | 1981-12-08 | Mcdonnell Douglas Corporation | Method of fabricating metallic sandwich structure |
DE19845374C2 (de) * | 1998-10-02 | 2003-01-02 | Swg Metallverarbeitung Und Mon | Verfahren zum Herstellen von Kühlkörpern für elektrische und/oder elektronische Bauteile |
SE512942C2 (sv) * | 1998-10-02 | 2000-06-12 | Volvo Aero Corp | Förfarande för tillverkning av utloppsmunstycken för raketmotorer |
US6138898A (en) * | 1998-12-22 | 2000-10-31 | The Boeing Company | Corner gap weld pattern for SPF core packs |
US6976082B1 (en) * | 2000-11-03 | 2005-12-13 | At&T Corp. | System and method for receiving multi-media messages |
DE60226574D1 (de) | 2001-01-11 | 2008-06-26 | Volvo Aero Corp | Verfahren zur herstellung von austrittsdüsen für raketentriebwerke |
ATE393875T1 (de) * | 2001-01-11 | 2008-05-15 | Volvo Aero Corp | Raketentriebwerksglied und ein verfahren zur herstellung eines raketentriebwerksglieds |
US7596940B2 (en) | 2005-03-22 | 2009-10-06 | Pratt & Whitney Rocketdyne, Inc. | Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing |
DE102008011502A1 (de) * | 2008-02-25 | 2009-09-03 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Düsenerweiterung und Verfahren zur Herstellung einer Düsenerweiterung |
-
2010
- 2010-02-08 DE DE102010007272.9A patent/DE102010007272B4/de not_active Expired - Fee Related
-
2011
- 2011-01-24 US US13/012,215 patent/US20110192137A1/en not_active Abandoned
- 2011-02-07 EP EP11000944.6A patent/EP2354518B1/fr active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3613207A (en) * | 1969-06-05 | 1971-10-19 | Messerschmitt Boelkow Blohm | Method for covering and closing cooling channels of a combustion chamber |
FR2311608A2 (fr) * | 1975-05-22 | 1976-12-17 | Messerschmitt Boelkow Blohm | Procede de realisation de pieces de revolution, notamment refroidies par un liquide, comme des tuyeres et chambres de combustion pour moteurs-fusees |
FR2774432A1 (fr) * | 1998-02-04 | 1999-08-06 | Daimler Benz Ag | Chambre de combustion pour des moteurs et des tuyeres de forte puissance |
WO2000032920A1 (fr) * | 1998-11-27 | 2000-06-08 | Volvo Aero Corporation | Structure tuyere pour cols de tuyeres avec paroi refroidie |
US6998570B1 (en) * | 2004-11-04 | 2006-02-14 | United Technologies Corporation | Beam welding apparatus and methods |
US20070259192A1 (en) * | 2006-05-08 | 2007-11-08 | Eads Space Transportation Gmbh | Method for producing components for rocket construction |
Also Published As
Publication number | Publication date |
---|---|
DE102010007272A1 (de) | 2011-08-11 |
EP2354518B1 (fr) | 2014-11-05 |
DE102010007272B4 (de) | 2016-09-15 |
EP2354518A2 (fr) | 2011-08-10 |
US20110192137A1 (en) | 2011-08-11 |
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